On plane stress-plane strain interactions in fatigue crack growth

International Journal of Fatigue

Volumn 20, Issue 6, 1998, Pages 441-448

  Bao, H ^a,b   McEvily, A J ^a  

^a UNIVERSITY OF CONNECTICUT   (United States)

^b PRATT AND WHITNEY   (United States)

Author keywords

Aluminium alloys; Crack closure; Fatigue crack growth; Steel

Indexed keywords

ALUMINUM ALLOYS; CRACK PROPAGATION; STEEL; STRAIN; STRESSES;

CRACK CLOSURE; FATIGUE CRACK GROWTH;

FATIGUE TESTING;

EID: 0032114733     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(98)00013-9     Document Type: Article

References (7)

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2. Ryder, D. A., Discussion of paper by Yokobori et al. in Fracture 1969. In Fracture 1969, Brighton, England. Chapman and Hall, London, 1969, pp. 932-933.
3. Kikukawa, M., Jono, M. and Tanaka, K., Fatigue crack closure behavior at low stress intensity level. Proc. Second Int. Conf. on Mechanical Behavior of Materials. ASM, Metals Park, OH, 1976, pp. 716-720.
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6. McEvily, A. J. and Yang, Z., The nature of the two opening levels following an overload in fatigue crack growth. Metall. Trans. A, 1989, 21A, 2717-2727.
7. Davidson, D. L. and Lankford, J., Fatigue crack tip mechanics of a powder metallurgy aluminum alloy in vacuum and humid air. Fatigue Engng Mater. Struct., 1984, 7, 29-39.